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TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME

United States Patent Application

20130318976
A1
View the Complete Application at the US Patent & Trademark Office
A turbomachine combustor nozzle includes a first plate member having a first plurality of openings, and a second plate member having a second plurality of openings that are configured and disposed to be in alignment with the first plurality of openings. A plurality of nozzle members extends through corresponding ones of the first plurality of openings and the second plurality of openings. Each of the plurality of nozzle members includes a solid core.
Melton, Patrick Benedict (Horse Shoe, NC), Stoia, Lucas John (Taylors, SC), Westmoreland, James Harold (Greer, SC)
GENERAL ELECTRIC COMPANY (Schenectady NY)
13/ 482,584
May 29, 2012
FEDERAL RESEARCH STATEMENT [0001] This invention was made with Government support under Contract Number DE-FC26-05NT42643 awarded by the Department Of Energy. The Government has certain rights in this invention.